dc.contributor.authorGoh, Shu Ting
dc.contributor.authorPasserello, Chris E
dc.contributor.authorAbdelkhalik, Ossama
dc.date.accessioned2013-08-06T04:20:11Z
dc.date.available2013-08-06T04:20:11Z
dc.date.copyright2010en_US
dc.date.issued2010
dc.identifier.citationGoh, S. T., Passerello, C. E., & Abdelkhalik, O. (2010). 2010 IEEE Aerospace Conference. Spacecraft Relative Attitude Determination, 1-6.en_US
dc.identifier.urihttp://hdl.handle.net/10220/13047
dc.description.abstractA method to determine the relative attitudes between three spacecraft is developed. The method requires four direction measurements between the three spacecraft. The simulation results and covariance analysis show that the method's error falls within a three sigma boundary without exhibiting any singularity issues. A study of the accuracy of the proposed method with respect to the shape of the spacecraft formation is also presented.en_US
dc.language.isoenen_US
dc.rights© 2010 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. The published version is available at DOI: [http://dx.doi.org/10.1109/AERO.2010.5446994].en_US
dc.subjectDRNTU::Engineering::Electrical and electronic engineering
dc.titleSpacecraft relative attitude determinationen_US
dc.typeConference Paper
dc.contributor.conferenceIEEE Aerospace Conference (2010 : Montana, US)en_US
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen_US
dc.identifier.doihttp://dx.doi.org/10.1109/AERO.2010.5446994
dc.description.versionAccepted versionen_US
dc.identifier.rims167984


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